airplanedrawing220.pdf
TRANSCRIPT
1870.54960.00
2598.97
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CHARACTERISTICS DATA OF AIRCRAFT - 220
ITEM Wing Horizontal Tail Vertical Tail
AirfoilWhitcomb
Integral Supercritica
l AirfoilTR-51 NACA -
0009
Area(Sq ft) 2211.82 470.13 222.17Aspect Ratio 7 3.5 1.2
Sweep Angle (deg) 30 30 30
Dihedral Angle (deg) 7.03 7.05 --
Volume Coefficient -- 1.10 0.08
PAYLOAD CAPACITY Passengers - 220
Class# of
Seats Abreasts
# Seats Seat Pitch
First Class 4 20 40"Econom
y 7 200 33"
Cargo Container Type LD-2/LD-3ALocation Volume # of
ContainersFrontAft
D
C
B
A
B
C
D
12345678
8 7 6 5 4 3 2 1
E
F
E
F
3-View Solidbody A_220 Aircraft
SHEET 1 OF 1
6/6/14
6/6/14
6/6/14
6/6/14
6/6/14J. Mok
J. Mok
J. Mok
J. Mok
Jin Mok
UNLESS OTHERWISE SPECIFIED:
SCALE: 1:384WEIGHT:
REVDWG. NO.
CSIZE
TITLE:
NAME DATE
COMMENTS:
Q.A.
MFG APPR.
ENG APPR.
CHECKED
DRAWN
FINISH
MATERIAL
INTERPRET GEOMETRICTOLERANCING PER:
DIMENSIONS ARE IN INCHESTOLERANCES:FRACTIONALANGULAR: MACH BEND TWO PLACE DECIMAL THREE PLACE DECIMAL
APPLICATION
USED ONNEXT ASSY
PROPRIETARY AND CONFIDENTIALTHE INFORMATION CONTAINED IN THISDRAWING IS THE SOLE PROPERTY OF<INSERT COMPANY NAME HERE>. ANY REPRODUCTION IN PART OR AS A WHOLEWITHOUT THE WRITTEN PERMISSION OF<INSERT COMPANY NAME HERE> IS PROHIBITED.
A
DO NOT SCALE DRAWING